EA021815B1 - Life-saving vehicle - Google Patents

Life-saving vehicle Download PDF

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Publication number
EA021815B1
EA021815B1 EA201390002A EA201390002A EA021815B1 EA 021815 B1 EA021815 B1 EA 021815B1 EA 201390002 A EA201390002 A EA 201390002A EA 201390002 A EA201390002 A EA 201390002A EA 021815 B1 EA021815 B1 EA 021815B1
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EA
Eurasian Patent Office
Prior art keywords
vehicle
rotor
blades
vehicle according
stabilizing
Prior art date
Application number
EA201390002A
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Russian (ru)
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EA201390002A1 (en
Inventor
Ян-Эверт Линдмарк
Юхани Нииниваара
Original Assignee
Велл-Хэд Рескью Аб
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Application filed by Велл-Хэд Рескью Аб filed Critical Велл-Хэд Рескью Аб
Publication of EA201390002A1 publication Critical patent/EA201390002A1/en
Publication of EA021815B1 publication Critical patent/EA021815B1/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/02—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement
    • B63B1/04—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with single hull
    • B63B1/041—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with single hull with disk-shaped hull
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/02—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement
    • B63B1/04—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with single hull
    • B63B1/047—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with single hull with spherical hull or hull in the shape of a vertical ring
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B39/00—Equipment to decrease pitch, roll, or like unwanted vessel movements; Apparatus for indicating vessel attitude
    • B63B39/06—Equipment to decrease pitch, roll, or like unwanted vessel movements; Apparatus for indicating vessel attitude to decrease vessel movements by using foils acting on ambient water
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/52—Skis or runners
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/08—Helicopters with two or more rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/473—Constructional features
    • B64C27/50—Blades foldable to facilitate stowage of aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/52—Tilting of rotor bodily relative to fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface  specially adapted for helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8263—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like
    • B64C2027/8281—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like comprising horizontal tail planes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/55—UAVs specially adapted for particular uses or applications for life-saving or rescue operations; for medical use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U60/00—Undercarriages
    • B64U60/10—Undercarriages specially adapted for use on water

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Vehicle Body Suspensions (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Body Structure For Vehicles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Emergency Lowering Means (AREA)
  • Wind Motors (AREA)
  • Braking Arrangements (AREA)

Abstract

The invention concerns a lifesaving vehicle (10) designed as a hollow body with the form of a sphere or disk essentially flattened along a vertical axis (16) that demonstrates its greatest width in a horizontal plane (15) and which body, composed of an upper part (11) and a lower part (13), limits an internal passenger compartment (25), whereby the body comprises a stabilizing arrangement (12) that stabilizes the vehicle when it is in water, a telescopic arrangement (40), a stabilization means (14) arranged at the lower part, which stabilization means can be displaced in a vertical direction downwards from the lower part through activation of the telescopic arrangement (40). The vehicle, in order for it to travel not only in the air but also in water, comprises: a first and second rotor (52, 17), a motor (55) with an associated transmission (54), a pair of propulsion units (60) and a stabilizing fin (65).

Description

(57) Изобретение относится к спасательному транспортному средству (10), выполненному как пустотелый корпус, имеющий форму, по существу, диска или сферы, сплюснутой вдоль вертикальной оси (16), и имеющей наибольшую ширину в горизонтальной плоскости (15), при этом корпус содержит верхнюю часть (11) и нижнюю часть (13), ограничивает внутренний пассажирский отсек (25), при этом корпус содержит стабилизирующую конструкцию (12), которая стабилизирует транспортное средство, находящееся в воде, телескопическую конструкцию (40), стабилизирующее средство (14), расположенное на нижней части, при этом стабилизирующее средство выполнено с возможностью смещения в вертикальном направлении вниз от нижней части за счет активации телескопической конструкции (40). Для того чтобы транспортное средство могло двигаться не только в воздухе, но и по воде, оно содержит первый и второй роторы (52, 17), двигатель (55) с соединенной трансмиссией (54), пару двигательных установок (60) и стабилизатор(57) The invention relates to a rescue vehicle (10), made as a hollow body, having the shape of a substantially disk or sphere, flattened along the vertical axis (16), and having the largest width in the horizontal plane (15), while the body contains the upper part (11) and the lower part (13), limits the inner passenger compartment (25), while the housing contains a stabilizing structure (12) that stabilizes the vehicle in water, a telescopic structure (40), stabilizing means (14 ), rasp laid on the lower part, while the stabilizing means is made with the possibility of displacement in the vertical direction down from the lower part due to the activation of the telescopic structure (40). In order for the vehicle to move not only in air but also through water, it contains the first and second rotors (52, 17), an engine (55) with a connected transmission (54), a couple of propulsion systems (60) and a stabilizer

Claims (10)

1. Спасательное транспортное средство (10), выполненное в форме пустотелого корпуса лодки в форме сферы или диска, по существу, сплющенного вдоль вертикальной оси (16), который имеет наибольшую ширину в горизонтальной плоскости (15), при этом корпус состоит из верхней части (11) и нижней части (13) и ограничивает внутренний пассажирский отсек (25), при этом корпус содержит стабилизирующую конструкцию (12) с поплавковой камерой, выполненной в форме цилиндра, который, проходя вокруг самой широкой части или центра транспортного средства, стабилизирует транспортное средство, когда оно находится в воде, телескопическую конструкцию (40), расположенную центрально в корпусе и проходящую вертикально сквозь корпус, выполненную как внутренний цилиндрический кожух, сформированный из круглых цилиндрических труб (40:1-40:п), вставленных телескопически друг в друга, стабилизирующее средство (14), расположенное на нижней части и содержащее, по существу, дисковидный узел, который отходит радиально от вертикальной оси (16) транспортного средства, при этом стабилизирующее средство выполнено с возможностью смещения в вертикальном направлении вниз от нижней части с помощью активации телескопической конструкции (40), отличающееся тем, что для движения не только в воздухе, но и по воде, содержит первый и второй роторы (52, 17), установленные для вращения вокруг первой и второй осей (16, 16'), соответственно в противоположных направлениях, при этом один ротор (52) расположен так, чтобы отходить от верхней части (11) транспортного средства, а второй ротор (17) расположен так, чтобы отходить от нижней части (13) транспортного средства, при этом первый ротор содержит набор лопастей (52), которые отходят в первой плоскости (Р53) лопастей, а второй ротор содержит множество лопастей (18), которые отходят во второй плоскости (Р18) лопастей;1. Rescue vehicle (10), made in the form of a hollow boat hull in the form of a sphere or disk, essentially flattened along the vertical axis (16), which has the greatest width in the horizontal plane (15), while the hull consists of the upper part (11) and the lower part (13) and limits the inner passenger compartment (25), while the housing contains a stabilizing structure (12) with a float chamber made in the form of a cylinder, which, passing around the widest part or center of the vehicle, stabilizes ansport means, when it is in water, a telescopic structure (40) located centrally in the body and extending vertically through the body, made as an inner cylindrical casing formed of round cylindrical tubes (40: 1-40: p) inserted telescopically into each other other, stabilizing means (14) located on the lower part and containing a substantially disk-like assembly that extends radially from the vertical axis (16) of the vehicle, while the stabilizing means is arranged to see The buildings in the vertical direction down from the bottom by activating the telescopic structure (40), characterized in that for movement not only in air but also in water, contains the first and second rotors (52, 17) installed for rotation around the first and the second axles (16, 16 '), respectively, in opposite directions, while one rotor (52) is located so as to depart from the upper part (11) of the vehicle, and the second rotor (17) is located so as to depart from the lower part ( 13) a vehicle, wherein the first rotor comprises n the collection of blades (52), which extend in the first plane (P53) of the blades, and the second rotor contains many blades (18), which extend in the second plane (P18) of the blades; двигатель (55), поддерживаемый транспортным средством вместе с соединенной с ним трансмиссией (54) для приведения во вращение первого и второго роторов (52, 17) и генерирования вертикальной подъемной силы в среде, которая окружает транспортное средство, при этом такая среда может быть воздухом или водой;an engine (55) supported by the vehicle together with a transmission (54) connected to it to drive the first and second rotors (52, 17) and generate vertical lift in the environment that surrounds the vehicle, and this environment may be air or water; пару двигательных установок (60), установленных на диаметрально противоположных сторонах корпуса для горизонтального движения транспортного средства;a pair of propulsion systems (60) mounted on diametrically opposite sides of the housing for horizontal movement of the vehicle; стабилизатор (65), отходящий радиально от внешней периферии транспортного средства и оснащенный рулями (66) направления и рулями (67) высоты для маневрирования транспортным средством под действием набегающих потоков среды.a stabilizer (65) radially extending from the outer periphery of the vehicle and equipped with rudders (66) of the direction and rudders (67) of height for maneuvering the vehicle under the action of incident media flows. 2. Транспортное средство по п.1, в котором двигатель (55), поддерживаемый транспортным средством, и соединенная с ним трансмиссия (54) расположены вдоль вертикальной оси (16) в отсеке между первым и вторым роторами (52, 17).2. The vehicle according to claim 1, in which the engine (55) supported by the vehicle and the transmission (54) connected to it are located along the vertical axis (16) in the compartment between the first and second rotors (52, 17). 3. Транспортное средство по п.1 или 2, в котором каждая из двух двигательных установок (60) содержит реактивный двигатель, предназначенный для создания реактивной струи.3. The vehicle according to claim 1 or 2, in which each of the two propulsion systems (60) contains a jet engine designed to create a jet stream. 4. Транспортное средство по п.3, в котором каждая двигательная установка содержит средство (61) для управления направлением выходного потока реактивного двигателя.4. The vehicle according to claim 3, in which each propulsion system comprises means (61) for controlling the direction of the output stream of the jet engine. 5. Транспортное средство по п.4, в котором управляющее средство содержит управляющую створку (62), которая выполнена с возможностью поворачиваться вокруг соответствующей горизонтальной оси5. The vehicle according to claim 4, in which the control means comprises a control leaf (62), which is configured to rotate around the corresponding horizontal axis - 5 021815 (63) под действием управляющего и приводного средства.- 5 021815 (63) under the influence of control and drive means. 6. Транспортное средство по любому из пп.1-5, в котором каждая из лопастей (53), являющихся компонентами первого ротора (52), шарнирно закреплена на верхней части (11) транспортного средства и, начиная из выдвинутого положения, в котором лопасти проходят в плоскости (Р53) лопастей, выполнены с возможностью перевода в неактивное положение под действием конструкции (81), содержащей поршень и цилиндр, которая работает между каждой лопастью и верхней частью, складываясь совместно внутрь и вниз к той стороне верхней части, которая обращена вверх.6. The vehicle according to any one of claims 1 to 5, in which each of the blades (53), which are components of the first rotor (52), are pivotally mounted on the upper part (11) of the vehicle and, starting from the extended position, in which the blades pass in the plane (P53) of the blades, are made with the possibility of moving to an inactive position under the action of a structure (81) containing a piston and a cylinder that works between each blade and the upper part, folding together inward and down to the side of the upper part that faces up . 7. Транспортное средство по любому из пп.1-6, в котором стабилизирующее средство (14) на нижней стороне, обращенной вниз, содержит множество поддерживающих ног (19), выполненных с возможностью опускания и каждая из которых шарнирно прикреплена к механизму, расположенному на нижней части (21) стабилизирующего средства и, начиная из сложенного, неактивного положения, в котором поддерживающие ноги проходят параллельно обращенной вниз стороне стабилизирующего средства (14) и вдоль нее, выполнены с возможностью перевода в активное положение под действием механизма (22), содержащего поршень и цилиндр, который является компонентом стабилизирующего средства, и так, чтобы транспортное средство могло опираться на опорные ноги, когда оно находится на суше.7. The vehicle according to any one of claims 1 to 6, in which the stabilizing means (14) on the lower side, facing down, contains many supporting legs (19), made with the possibility of lowering and each of which is pivotally attached to a mechanism located on the lower part (21) of the stabilizing means and, starting from the folded, inactive position, in which the supporting legs extend parallel to and along the side of the stabilizing means (14) facing downward, are made with the possibility of transition to the active position under the deis viem mechanism (22) comprising a piston and cylinder, which is a component of a stabilizing agent, and so that the vehicle can rest on the supporting legs when it is on land. 8. Транспортное средство по любому из пп.1-7, в котором круглые цилиндрические трубы (40:140:п) телескопической конструкции (40), телескопически вставленные одна в другую, расположены так, чтобы при активации телескопической конструкции не только первый ротор (52), расположенный на верхней части (11), но и стабилизирующее средство (14), расположенное на нижней части (13), если смотреть из его убранного положения, смещались на некоторое расстояние от корпуса вдоль соответствующей оси (16, 16').8. A vehicle according to any one of claims 1 to 7, in which round cylindrical pipes (40: 140: p) of a telescopic structure (40) telescopically inserted one into another are arranged so that when the telescopic structure is activated, not only the first rotor ( 52) located on the upper part (11), but also the stabilizing means (14) located on the lower part (13), when viewed from its retracted position, were displaced by a certain distance from the body along the corresponding axis (16, 16 '). 9. Транспортное средство по п.8, в котором второй ротор (17) установлен в отсеке, который ограничен между стабилизирующим средством (14) и нижней частью (13) корпуса, когда ротор расположен в убранном положении у нижней части (13).9. The vehicle of claim 8, in which the second rotor (17) is installed in the compartment, which is limited between the stabilizing means (14) and the lower part (13) of the housing, when the rotor is located in the retracted position at the lower part (13). 10. Транспортное средство по любому из пп.1-8, в котором первый ротор (52) установлен в свободно плавающем состоянии в несущем гнезде (73) с возможностью занятия различных угловых положений (А) относительно горизонтальной плоскости под действием множества электрических механизмов (76), содержащих поршень и цилиндр, которые шарнирно установлены между ротором и фиксированным несущим корпусом (77), который поддерживает несущее гнездо.10. A vehicle according to any one of claims 1 to 8, in which the first rotor (52) is mounted in a free-floating state in the carrier socket (73) with the possibility of occupying various angular positions (A) relative to the horizontal plane under the action of many electrical mechanisms (76 ), containing a piston and a cylinder, which are pivotally mounted between the rotor and the fixed bearing housing (77), which supports the bearing socket. Фиг. 1FIG. one
EA201390002A 2010-06-08 2011-06-07 Life-saving vehicle EA021815B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE1050584A SE535346C2 (en) 2010-06-08 2010-06-08 survival craft
PCT/SE2011/050696 WO2011155892A1 (en) 2010-06-08 2011-06-07 Life-saving vehicle

Publications (2)

Publication Number Publication Date
EA201390002A1 EA201390002A1 (en) 2013-06-28
EA021815B1 true EA021815B1 (en) 2015-09-30

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EA201390002A EA021815B1 (en) 2010-06-08 2011-06-07 Life-saving vehicle

Country Status (12)

Country Link
US (1) US8919691B2 (en)
EP (1) EP2580118A1 (en)
JP (1) JP5807060B2 (en)
KR (1) KR20130124937A (en)
CN (1) CN103003148B (en)
AU (1) AU2011262543B8 (en)
CA (1) CA2802027A1 (en)
EA (1) EA021815B1 (en)
MX (1) MX2012014436A (en)
MY (1) MY159133A (en)
SE (1) SE535346C2 (en)
WO (1) WO2011155892A1 (en)

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CA2815885C (en) * 2013-05-15 2018-05-15 Draganfly Innovations Inc. Compact unmanned rotary aircraft
CN103640675B (en) * 2013-12-18 2016-05-04 江苏科技大学 The amphibious unmanned boat of water surface trisome
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